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1.3 A Brief Description of the 777 Family of Airplanes

777-200/-200ER Airplane

The 777-200/-200ER is a twin-engine airplane designed for medium to long range flights. It is

powered by advanced high bypass ratio engines. Characteristics unique to the 777 include:

Two-crew cockpit with digital avionics

Circular cross-section

Lightweight aluminum and composite alloys

Structural carbon brakes

Six-wheel main landing gears

Main gear aft axle steering

High bypass ratio engines

Fly-by-wire system

777-200LR Airplane

The 777-200LR is a derivative of the 777-200 airplane and is equipped with raked wingtips to

provide additional cruise altitude and range. It is powered by high bypass ratio engines that develop

higher thrusts than those used in the 777-200/-200ER airplanes. The 777-200LR has an identical

fuselage as the 777-200/-200ER but has a wider wingspan due to raked wingtips.

777-300 Airplane

The 777-300 is a second-generation derivative of the 777-200. Two body sections are added to the

fuselage to provide additional passenger seating and cargo capacity.

777-300ER Airplane

The 777-300ER is a derivative of the 777-300 airplane and is equipped with raked wingtips for

additional cruise altitude and range. It is powered by high bypass ratio engines that develop higher

thrusts than those used in the 777-200/-200ER/-300 airplanes. The 777-300ER has an identical

fuselage as the 777-300, but has a wider wingspan due to the raked wingtips.

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777-Freighter Airplane

The 777-Freighter, newest member of the 777 Family of airplanes, is based on the 777-200LR

Worldliner (Longer Range) passenger airplane. The 777-Freighter will fly farther than any other

freighter, providing more capacity than any other twin-engine freighter, and will meet QC2 noise

standards for maximum accessibility to noise-sensitive airports. The 777-Freighter will share the

777 Family’s advanced features of a state-of-the-art flight deck, fly-by-wire design and an advanced

wing design, including raked wing tips. The 777-Freighter is powered by the world’s most powerful

commercial jet engine, General Electric’s GE90-110B1L.

The 777-Freighter is designed to integrate smoothly with existing cargo operations and facilitate

interlining with 747 freighter fleets. Cargo operators will be able to easily transfer 10-foot-high

pallets between the two models via the large main deck cargo door.

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Main Gear Aft Axle Steering

The main gear axle steering is automatically engaged based on the nose gear steering angle. This

allows for less tire scrubbing and easier maneuvering into gates with limited parking clearances.

High Bypass Ratio Engines

The 777 airplane is powered by two high bypass ratio engines. The following table shows the

available engine options.

ENGINE ENGINE ENGINE MAX TAXI WEIGHT (LB)

MANUFACTURER MODEL THRUST 777-200LR 777-300ER 777F

GGEENNEERRAALL GGEE9900--111100BB 111100,,000000 LLBB 776688,,000000 -- --

EELLEECCTTRRIICC GGEE9900--111100BB11 111100,,000000 LLBB 776688,,000000 -- --

G

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9

9

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Document Applicability

This document contains data specific to the 777-200LR, 777-300ER and 777-Freighter.

Data for the 777-200, 777-200ER, and 777-300 airplanes are contained in document D6-58329.

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2.0 AIRPLANE DESCRIPTION

2.1 General Characteristics

Maximum Design Taxi Weight (MTW). Maximum weight for ground maneuver as limited by

aircraft strength and airworthiness requirements. (It includes weight of taxi and run-up fuel.)

Maximum Design Takeoff Weight (MTOW). Maximum weight for takeoff as limited by aircraft

strength and airworthiness requirements. (This is the maximum weight at start of the takeoff run.)

Maximum Design Landing Weight (MLW). Maximum weight for landing as limited by aircraft

strength and airworthiness requirements.

Maximum Design Zero Fuel Weight (MZFW). Maximum weight allowed before usable fuel and

other specified usable agents must be loaded in defined sections of the aircraft as limited by strength

and airworthiness requirements.

Operating Empty Weight (OEW). Weight of structure, powerplant, furnishing systems, unusable

fuel and other unusable propulsion agents, and other items of equipment that are considered an

integral part of a particular airplane configuration. Also included are certain standard items,

personnel, equipment, and supplies necessary for full operations, excluding usable fuel and payload.

Maximum Structural Payload. Maximum design zero fuel weight minus operational empty weight.

Maximum Seating Capacity. The maximum number of passengers specifically certificated or

anticipated for certification.

Maximum Cargo Volume. The maximum space available for cargo.

Usable Fuel. Fuel available for aircraft propulsion.

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CHARACTERISTICS UNITS 777-200LR 777-300ER 777-F

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2.1.1 GENERAL CHARACTERISTICS

MM OO DD EE LL 77 77 77 -- 22 00 00 LLRR .. -- 33 00 00 EE RR ,, 77 77 77 FF

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2.2.1 GENERAL DIMENSIONS

MM OO DD EE LL 77 77 77 -- 22 00 00 LLRR

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MM oo dd ee ll 77 77 77 -- 33 00 00 EE RR

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MM OO DD EE LL 77 77 77 FF

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3.0 AIRPLANE PERFORMANCE

3.1 General Information

3.2 Payload/Range for 0.84 Mach Cruise

3.3 F.A.R. Takeoff Runway Length Requirements

3.4 F.A.R. Landing Runway Length Requirements

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3.2.1 PAYLOAD/RANGE FOR 0.84 MACH CRUISE

MM OO DD EE LL 77 77 77 -- 22 00 00 LLRR (( GG EE 9 9 00 -- 11 00 00 SS EE RR II EE SS EE NN GG II NN EE SS ) )

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MM OO DD EE LL 77 77 77 -- 33 00 00 EE RR (( GG EE 9 9 00 -- 11 11 55 BB LL EE NN GG II NN EE SS ) )

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MM OO DD EE LL 77 77 77 FF (( GG EE 9 9 00 -- 11 00 00 SS EE RR II EE SS EE NN GG II NN EE SS ) )

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3.3.1 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS - STANDARD DAY

MM OO DD EE LL 77 77 77 -- 22 00 00 LLRR (( GG EE 9 9 00 -- 11 11 00 BB 11 LL EE NN GG II NN EE SS ) )

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3.3.2 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS STANDARD DAY +27oF (STD + 15oC)


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3.3.3 TAKEOFF RUNWAY LENGTH REQUIREMENTS STANDARD DAY +49oF (STD + 27oC)


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MM OO DD EE LL 77 77 77 -- 22 00 00 LLRR (( GG EE 9 9 00 -- 11 11 55 BB LL EE NN GG II NN EE SS ) )

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3.3.7 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS - STANDARD DAY+49oF (STD + 27oC)


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MM OO DD EE LL 77 77 77 FF (( GG EE 9 9 00 -- 11 11 00 BB 11 LL EE NN GG II NN EE SS ) )

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3.3.14 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS - STANDARD DAY + 27°F (STD + 15oC)


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3.3.17 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS STANDARD DAY

MM OO DD EE LL 77 77 77 FF (( GG EE 9 9 00 -- 11 11 55 BB LL EE NN GG II NN EE SS ) )

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3.3.18 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS STANDARD DAY + 27°F (STD + 15° C)


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3.4.1 F.A.R. LANDING RUNWAY LENGTH REQUIREMENTS – FLAPS 25


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